Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe523-il-100000 Airfoil,goe523-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,48.7647 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe523-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.250,0.0754,0.11636,0.11173,-0.0953,0.8453,0.1111 -7.000,0.0419,0.11818,0.11363,-0.0919,0.8314,0.1123 -6.750,0.0076,0.11990,0.11542,-0.0889,0.8195,0.1127 -6.500,0.0637,0.11176,0.10722,-0.0906,0.8178,0.1157 -6.250,0.0872,0.10849,0.10392,-0.0920,0.8139,0.1199 -6.000,0.0791,0.10777,0.10324,-0.0898,0.8050,0.1224 -5.750,0.0621,0.10761,0.10311,-0.0886,0.7966,0.1257 -5.500,0.0232,0.10951,0.10510,-0.0860,0.7833,0.1269 -5.250,0.0368,0.10507,0.10065,-0.0885,0.7792,0.1286 -5.000,0.0737,0.10060,0.09613,-0.0876,0.7776,0.1316 -4.750,0.0529,0.10096,0.09656,-0.0823,0.7650,0.1326 -4.500,0.0732,0.09788,0.09345,-0.0848,0.7614,0.1378 -4.250,0.0565,0.09748,0.09309,-0.0981,0.7469,0.1440 -4.000,0.0726,0.09358,0.08917,-0.0914,0.7445,0.1456 -3.750,0.0646,0.09308,0.08873,-0.0862,0.7346,0.1470 -3.500,0.1137,0.08855,0.08408,-0.1069,0.7285,0.1616 -3.250,0.1242,0.08545,0.08100,-0.0992,0.7263,0.1634 -3.000,0.1938,0.07964,0.07503,-0.1180,0.7245,0.1800 -2.750,0.4318,0.05143,0.04523,-0.1893,0.7271,0.1123 -2.500,0.5211,0.04564,0.03892,-0.2029,0.7268,0.1076 -2.250,0.5648,0.04414,0.03692,-0.2083,0.7182,0.1069 -2.000,0.6220,0.04199,0.03427,-0.2138,0.7145,0.1105 -1.750,0.6806,0.03953,0.03151,-0.2185,0.7129,0.1158 -1.500,0.7364,0.03732,0.02913,-0.2221,0.7117,0.1234 -1.250,0.7943,0.03511,0.02685,-0.2261,0.7105,0.1389 -1.000,0.8569,0.03271,0.02453,-0.2309,0.7096,0.1747 -0.750,0.8745,0.03317,0.02526,-0.2301,0.6992,0.2256 -0.500,0.9296,0.03177,0.02407,-0.2340,0.6962,0.3298 -0.250,0.9844,0.03048,0.02293,-0.2371,0.6938,0.4122 0.000,1.0418,0.02940,0.02188,-0.2403,0.6915,0.4755 0.250,1.0372,0.03070,0.02325,-0.2349,0.6795,0.4953 0.500,1.0880,0.02984,0.02233,-0.2372,0.6760,0.5325 0.750,1.1473,0.02884,0.02118,-0.2411,0.6729,0.5639 1.000,1.1401,0.03007,0.02247,-0.2354,0.6608,0.5774 1.250,1.1976,0.02918,0.02139,-0.2395,0.6566,0.6074 1.500,1.1999,0.03012,0.02238,-0.2352,0.6463,0.6215 1.750,1.2451,0.02963,0.02174,-0.2376,0.6404,0.6488 2.000,1.2726,0.02972,0.02178,-0.2371,0.6333,0.6727 2.250,1.2904,0.03012,0.02216,-0.2354,0.6246,0.6946 2.500,1.3454,0.02936,0.02118,-0.2397,0.6196,0.7207 2.750,1.3422,0.03054,0.02247,-0.2349,0.6095,0.7342 3.000,1.3868,0.03012,0.02189,-0.2377,0.6034,0.7550 3.250,1.4048,0.03068,0.02243,-0.2363,0.5956,0.7716 3.500,1.4254,0.03105,0.02276,-0.2353,0.5879,0.7886 3.750,1.4808,0.03044,0.02191,-0.2400,0.5827,0.8108 4.000,1.4681,0.03185,0.02351,-0.2337,0.5735,0.8232 4.250,1.5043,0.03169,0.02324,-0.2352,0.5674,0.8447 4.500,1.5286,0.03189,0.02344,-0.2348,0.5611,0.8683 4.750,1.5230,0.03277,0.02451,-0.2295,0.5533,0.9068 5.000,1.5755,0.03248,0.02402,-0.2339,0.5478,1.0000 5.250,1.5778,0.03384,0.02545,-0.2305,0.5404,1.0000 5.500,1.5979,0.03454,0.02612,-0.2298,0.5336,1.0000 5.750,1.6619,0.03408,0.02540,-0.2361,0.5286,1.0000 6.000,1.6356,0.03621,0.02774,-0.2281,0.5210,1.0000 6.250,1.6630,0.03663,0.02810,-0.2284,0.5149,1.0000 6.500,1.7339,0.03595,0.02715,-0.2356,0.5103,1.0000 6.750,1.6859,0.03886,0.03038,-0.2245,0.5028,1.0000 7.000,1.7131,0.03929,0.03075,-0.2247,0.4972,1.0000 7.250,1.7871,0.03829,0.02948,-0.2320,0.4928,1.0000 7.500,1.7266,0.04201,0.03356,-0.2196,0.4853,1.0000 7.750,1.7527,0.04240,0.03391,-0.2196,0.4798,1.0000 8.000,1.8289,0.04100,0.03223,-0.2268,0.4755,1.0000 8.250,1.7561,0.04586,0.03749,-0.2136,0.4681,1.0000 8.500,1.7743,0.04672,0.03837,-0.2127,0.4627,1.0000 8.750,1.8422,0.04522,0.03667,-0.2180,0.4590,1.0000 9.000,1.7606,0.05182,0.04366,-0.2055,0.4514,1.0000 9.250,1.7551,0.05440,0.04633,-0.2024,0.4455,1.0000 9.500,1.8249,0.05196,0.04373,-0.2069,0.4425,1.0000 9.750,1.5513,0.08097,0.07351,-0.1865,0.4212,1.0000 10.000,1.6152,0.07629,0.06875,-0.1875,0.4210,1.0000 10.250,1.6929,0.07067,0.06302,-0.1897,0.4209,1.0000 10.500,1.8163,0.06206,0.05417,-0.1963,0.4216,1.0000 10.750,1.1569,0.16738,0.16088,-0.2013,0.3856,1.0000 11.000,1.0911,0.18219,0.17590,-0.2090,0.4164,1.0000